Path: Orbit/OrbitMechanics
% Calculates the orbit angular momentum given the input in equinoctial elements Since version 1. -------------------------------------------------------------------------- Form: h = HEq( eq ,mu ) -------------------------------------------------------------------------- ------ Inputs ------ eq Elements vector [a,P1,P2,Q1,Q2,L,K,l,n] mu Gravitational parameter ------- Outputs ------- h Angular momentum --------------------------------------------------------------------------
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